View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 39446U 13066AG 22136.14959564 .00001840 00000-0 24379-3 0 9990
2 39446 97.6834 101.6180 0068316 193.3501 166.5906 14.79451366456271
| Epoch (UTC): | 16 May 2022 03:35:25 |
| Eccentricity: | 0.0068316 |
| inclination: | 97.6834° |
| perigee height: | 583 km |
| apogee height: | 679 km |
| right ascension of ascending node: | 101.6180° |
| argument of perigee: | 193.3501° |
| revolutions per day: | 14.79451366 |
| mean anomaly at epoch: | 166.5906° |
| orbit number at epoch: | 45627 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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